When the cross-section of a nozzle increases continuously from entrance to exit, it is called a______________
A) convergent-divergent nozzle
B) divergent nozzle
C) convergent nozzle
D) none of the mentioned
Correct Answer:
Verified
Q7: De-Laval turbine is a_
A)multi rotor impulse turbine
B)impulse
Q8: The Parsons' reaction turbine has
A)only moving blades
B)only
Q9: What is the critical pressure ratio for
Q10: The ratio of the useful heat drop
Q11: Rateau turbine is_
A)pressure-velocity compounded turbine
B)simple reaction turbine
C)velocity
Q13: Aeroderivative engines have pressure ratios
A)greater than 30
B)lesser
Q14: Aeroderivative engines are larger.
Q15: Aeroderivative engines release higher emissions.
Q16: Critical pressure ratio is ratios of pressures
Q17: Ratio of critical pressure to inlet pressure
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